IT1178084B - COMPOSITE FUSELAGE FOR HELICOPTER - Google Patents
COMPOSITE FUSELAGE FOR HELICOPTERInfo
- Publication number
- IT1178084B IT1178084B IT47563/84A IT4756384A IT1178084B IT 1178084 B IT1178084 B IT 1178084B IT 47563/84 A IT47563/84 A IT 47563/84A IT 4756384 A IT4756384 A IT 4756384A IT 1178084 B IT1178084 B IT 1178084B
- Authority
- IT
- Italy
- Prior art keywords
- helicopter
- composite fuselage
- fuselage
- composite
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8301991 | 1983-01-25 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8447563A0 IT8447563A0 (en) | 1984-01-19 |
IT1178084B true IT1178084B (en) | 1987-09-09 |
Family
ID=10536903
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT47563/84A IT1178084B (en) | 1983-01-25 | 1984-01-19 | COMPOSITE FUSELAGE FOR HELICOPTER |
Country Status (4)
Country | Link |
---|---|
US (1) | US4531695A (en) |
DE (1) | DE3401189A1 (en) |
FR (1) | FR2539701B1 (en) |
IT (1) | IT1178084B (en) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2632604B1 (en) * | 1988-06-08 | 1991-07-12 | Aerospatiale | FRAME OF COMPOSITE MATERIAL IN PARTICULAR FOR AIRCRAFT FUSELAGE, AND METHOD FOR MANUFACTURING SAME |
DE3826636A1 (en) * | 1988-08-05 | 1990-02-08 | Messerschmitt Boelkow Blohm | COCKPIT, ESPECIALLY FOR A HELICOPTER |
JPH06255587A (en) * | 1993-03-09 | 1994-09-13 | Honda Motor Co Ltd | Aircraft |
DE4447740B4 (en) * | 1993-09-06 | 2008-10-09 | Sanyo Electric Co., Ltd., Moriguchi | Acoustic surface wave filter |
ES2112711B1 (en) * | 1994-05-25 | 1998-12-01 | Torres Martinez M | AIRCRAFT STRUCTURE. |
JP3888630B2 (en) * | 2002-12-04 | 2007-03-07 | 川崎重工業株式会社 | Energy absorbing member and helicopter impact resistant structure using the same |
ATE437275T1 (en) * | 2003-02-06 | 2009-08-15 | Swissfiber Ag | PLATE-SHAPED CONSTRUCTION ELEMENT |
FR2896770B1 (en) * | 2006-01-27 | 2008-04-11 | Eurocopter France | SIDE-HOLDING ANTI-CRASH COMPOSITE STRUCTURE FOR AIRCRAFT. |
FR2903961B1 (en) * | 2006-07-21 | 2009-09-25 | Eurocopter France | STRUCTURAL COMPONENT OF THE ROTOR CELL, METHOD FOR MANUFACTURING THE SAME, ROTARY CELL AND GIRAVION COMPRISING SUCH STRUCTURAL ELEMENTS |
RU2448865C2 (en) * | 2007-01-29 | 2012-04-27 | Эйрбас Оперейшнз, С.Л. | Aircraft mainframe made from composite material |
CN101715411A (en) * | 2007-01-29 | 2010-05-26 | 空客运营有限公司 | Aircraft loading frame by Composite Preparation |
FR2921899B1 (en) * | 2007-10-04 | 2011-04-15 | Airbus France | METHOD FOR LOCALLY REINFORCING COMPOSITE MATERIAL ELEMENT AND CENTRAL BOAT BOILER FOR REINFORCED AIRCRAFT |
FR2933066B1 (en) * | 2008-06-26 | 2010-09-10 | Airbus France | AIRCRAFT FUSELAGE ELEMENT |
JP4918567B2 (en) * | 2009-04-20 | 2012-04-18 | 三菱重工業株式会社 | Shock absorbing structure and manufacturing method thereof |
US8317135B2 (en) * | 2010-04-19 | 2012-11-27 | Sabreliner Corporation | Flexible mounting assembly for an air frame structure |
EP2404824B1 (en) | 2010-07-08 | 2015-09-09 | Airbus Opérations SAS | Aircraft structure and Method for producing such a structure |
US10099765B2 (en) * | 2012-08-08 | 2018-10-16 | The Boeing Company | Monolithic composite structures for vehicles |
FR3000018B1 (en) * | 2012-12-21 | 2016-12-09 | Airbus Operations Sas | AIRCRAFT FUSELAGE STIFFENER, ITS MANUFACTURING METHOD, AND AIRCRAFT FUSELAGE EQUIPPED WITH SUCH STIFFENER |
EP2889212B1 (en) * | 2013-12-30 | 2016-01-06 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Subfloor structure with an integral hull for a rotary wing aircraft |
PL2905228T3 (en) * | 2014-02-06 | 2018-05-30 | Airbus Helicopters Deutschland GmbH | Fuselage Airframe and Tank |
PL2979975T3 (en) * | 2014-07-30 | 2018-01-31 | Airbus Helicopters Deutschland GmbH | An aircraft with a framework structure that comprises at least one hollow frame. |
US10053203B2 (en) * | 2015-10-13 | 2018-08-21 | The Boeing Company | Composite stiffener with integral conductive element |
RU2694638C2 (en) * | 2017-11-09 | 2019-07-16 | Акционерное общество Научно-производственное объединение "Опытно-конструкторское бюро имени М.П. Симонова" | Fuselage caisson |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1966933A (en) * | 1931-06-25 | 1934-07-17 | Budd Edward G Mfg Co | Structural assembly and method of assembling the same |
US2604280A (en) * | 1944-09-12 | 1952-07-22 | Sncase | Hollow structural element for vehicles and more especially for aircraft |
CA928696A (en) * | 1970-10-30 | 1973-06-19 | C. Perazella John | Composite stringer and method of making it |
DE2639431A1 (en) * | 1976-09-02 | 1978-03-09 | Burkhart Dipl Ing Grob | Mountings in fibre reinforced plastic aircraft fuselages - using cast aluminium replacements for existing strength members |
US4113910A (en) * | 1977-04-27 | 1978-09-12 | Rockwell International Corporation | Composite load coupler for reinforcing composite structural joints |
-
1984
- 1984-01-14 DE DE19843401189 patent/DE3401189A1/en not_active Withdrawn
- 1984-01-17 US US06/571,456 patent/US4531695A/en not_active Expired - Fee Related
- 1984-01-19 IT IT47563/84A patent/IT1178084B/en active
- 1984-01-23 FR FR8400971A patent/FR2539701B1/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2539701A1 (en) | 1984-07-27 |
IT8447563A0 (en) | 1984-01-19 |
DE3401189A1 (en) | 1984-07-26 |
FR2539701B1 (en) | 1986-09-12 |
US4531695A (en) | 1985-07-30 |
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